JASC 5311
Service difficulty reports · 61,540
Reports filed under 5311 · Fuselage Main, Frame, 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 = '5311' 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 = '5311' 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 YENA2023113001506Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 20 AT FWD GALLEY AREA (1 EA) (CRACK INDICAT ION ON FRAME 20 LH SIDE AT UPPER JOGGLE AREA, HOLE 6, CRACK DIRECTION IS 3 OCLOCK AT FWD GALLEY AREA (1 EA); REF AEROMAN NR 2023-631085 WO 2023 358/1 ACCOMPLISHED RSDR DALA2023113009862Unknown · unknownSHIP 1602 ERA 613820-14AD ISSUED FOR REPAIR TO STA 303 LBL 10 FRAME WEB. A MOC REQUIRED. CORRECTIVE ACTION: AMOC TO AD 2021-10-19 REQUIRED NO LATER THAN 50000 TOTAL FLIGHT CYCLES / 34835 FLIGHT CYCLES FROM CURRENT HCK. (0084157)SDR DALA2023113009861Unknown · unknownSHIP 1602 ERA 613820-14 ISSUED FOR REPAIR AT STA 303, LBL 10 FRAME WEB. DT A DTE DAMAGE TOLERANCE ANALYSIS IS REQUIRED. CORRECTIVE ACTION: CORRECTION TO ABOVE, NOT TO EXCEED 22335 CYCLES FROM CURRENT HCK (0084152)SDR DALA2023112909817Unknown · unknownSHIP 0678 FUSELAGE / FRAME / RHS BSTA 1681 / WL 208 / S-17R & S-18R / CRACK INDICATION. CORRECTIVE ACTION: REF ERA 613080-14. (0084483)SDR DALA2023112909816Unknown · unknownSHIP 0678 FUSELAGE / FRAME / LHS BSTA 1681 / WL 208 / S-17L & S-18L / CRACK INDICATION. CORRECTIVE ACTION: REF ERA 613012-14. (0084402)SDR AALA202402296221Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME FACE AROUND FASTENER AT FR 35 AND S30L. REPAIRED FRAME PER EA 349944.SDR REXA2024010800051Frame · corroded"FS 533 FRAME IS CORRODED AT STGR 17L TO 18L. FABRICATED AND DRILLED ALL REPAIR PARTS IAW CRJ900 SRM 53-00-06-201-001-A03 STEP 6E-D-G FROM 7075-0 .080"" PO W91683, S1710-4, AND REPAIR FRAME SEGMENT P/N SH690-33121-5. INSTALLED A NEW SERVICEABLE FS 533 FRAME FRSDR YENA2023112901482Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 LH SIDE INTERCOSTAL FITTING ON OPEN FASTE NER HOLE 3, AT DOOR STOP FITTING 7 POSITION, CRACK DIRECTION IS 9 OCLO CK, AT FWD GALLEY AREA (1 EA); (RESOLVED ON W/O: 1249043 TASKCARD: NR-00032 ) REFERENCE AEROSDR YENA2023112901481Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 RH SIDE INTERCOSTAL FITTING ON OPEN FASTENER HOLE 3, AT DOOR STOP FITTING 7 POSITION, CRACK DIRECTION IS 3 OCLO CK, AT FWD GALLEY AREA (1 EA); (RESOLVED ON W/O: 1249043 TASKCARD: NR-00035 ) REFERENCE AEROMSDR YENA2023112901474Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 36 IN FWD CARGO COMPARTMENT (FR 36 LH, Y1523 PLUS 7.924 INCHES 2 EA ON UPPER SURFACE OF THE PRESSURE DECK CRACK INDICATION IS 7 AND 5 O CLOCK ); REF AEROMAN NR 2023-557157 WO 2023 275/1, ACCOMPLISHED MODIFICASDR YENA2023112901473Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 36 IN FWD CARGO COMPARTMENT (FR 36 LH Y1523 PLUS 7.044 INCHES ON UPPER SURFACE OF THE PRESSURE DECK, DIRECTION OF CRACK IS: 2 O CLOCK ); REF AEROMAN NR 2023-557158 WO 2023 275/1, ACCOMPLISHED MODIFICATION/REPSDR YENA2023112901472Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 36 IN FWD CARGO COMPARTMENT (FR 36 LH Y1523 PLUS 8.883 INCHES ON UPPER SURFACE OF THE PRESSURE DECK, DIRECTION OF CRACK IS: 4 O CLOCK ); REF AEROMAN NR 2023-557159 WO 2023 275/1, ACCOMPLISHED MODIFICATION/REPSDR YENA2023112901471Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 36 IN FWD CARGO COMPARTMENT (FR 36 RH -Y1523 PLUS 8.880 INCHES ON UPPER SURFACE OF THE PRESSURE DECK , DIRECTION O F CRACK IS: 6 O CLOCK ); REF AEROMAN NR 2023-557160 WO 2023 275/1, ACCOMPLISHED MODIFICATION/SDR YENA2023112901470Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 36 IN FWD CARGO COMPARTMENT (FR 36 RH -Y1523 PLUS 7.925 INCHES ON UPPER SURFACE OF THE PRESSURE DECK, DIRECTION O F CRACK IS: 6 O CLOCK ); REF AEROMAN NR 2023-557161 WO 2023 275/1, ACCOMPLISHED MODIFICATION/RSDR YENA2023112901469Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 36 IN FWD CARGO COMPARTMENT (FR 36 RH -Y1523 PLUS 7.045 INCHES ON UPPER SURFACE OF THE PRESSURE DECK, DIRECTION O F CRACK IS: 2 O CLOCK ); REF AEROMAN NR 2023-557162 WO 2023 275/1, ACCOMPLISHED MODIFICATION/RSDR YENA2023112901468Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 LH SIDE IN OPEN FASTENER HOLE A AT UPPER DOUBLE JOGGLE AREA, CRACK DIRECTION IS 3 OCLOCK, AT FWD GALLEY AREA ( 1 EA); REF AEROMAN N/R 2023- 556971, PERFORMED REPAIR AT FRAME 16 LH SIDE IN OPEN FASTENER HOLSDR DALA2023112809753Unknown · unknownCORROSION ON PREVIOUS SPLICE REPAIR ON FRAME STA 974 BTW LONG 30 AND 27 LH IN REF NRC 00216. SUMMARY OF NRC 00685: CORROSION LEVEL 2. PREVIOUS SPLICE REPAIR ON FRAME STA 974 BTW LONG 30 AND 27 LH WERE REPLACED AND INSTALLED PER B717-200 SRM 53-20-07-2R PROCEDUSDR SWAA2024010324786Frame · deformedCREASE ON FRAME BS196.5 BTW STR24R TO STR26R AT ELECTRONIC EQUIPMENT COMPARTMENT 2023-720016<[01] TOOL USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 25-JAN-23.;[02] REPLACED FRAME LOCATED ON BS196.5 BTW STR24R TO STR26R AT ELECTROSDR VNAA202401040032Frame · corrodedCORROSION ON FR 847+16.00 BTW STGR 26 LH/RH WAS FOUND. CORROSION ON FR 847+16.00 BTW STGR 26 LH/RH WAS EVALUATED OUT OF LIIMTS PER CRJ900 SRM 53-51-06-101-003-A05 AND WAS REPAIRED PER CRJ900 SRM 53-00-06-201-001-A03.SDR HNAA2024010300001Unknown · unknown53-2154 CRACKED FWD FUSELAGE 2, RH OVERHEADE SIDE FRAME ABOVE FLT DECK. R&R'D FRAME IAW EMB145 SRM 51-40-02SDR CALA2023112703479Frame · crackedREPAIR BEFORE NEXT FLIGHT, R/H FR 43 FOOT, REMOVED FASTENER HOLE HAS A CRACK INDICATION AT THE 3:O''CLOCK POS IN THE FRAME LAYER GEN BY V062335 ON HAECO LCQ NR 9294098/26098 (AD RELATED TASK) REPAIRED DISCREPANCY HOLE FR43 RH RAW DRAWING 15R3370233B .SDR AALA202403052155Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME HOLE D IN THE DOUBLE JOGGLE AREA OF DOOR STOP 7 AND FR 16 LEFT. REPAIRED FRAME PER EA 349691.SDR DALA2023112309663Unknown · unknownSHIP 3119 CRACK INDICATION WAS FOUND ON FR16LH AT HOLE IDENTIFIED AS HOLE #6. CORRECTIVE ACTION: REPAIRED PER ER/A 563227-14AD. (0078062)SDR DALA2023112309665Unknown · unknownSHIP 3119 CRACK INDICATION ON FRAME 16 RH SIDE CROSSBEAM SPLICING AREA. CORRECTIVE ACTION: REPAIRED PER ER/A 612478-14AD. (0077687)SDR DALA2023112309664Unknown · unknownSHIP 3119 CRACK INDICATION ON FRAME 20 LH SIDE CROSSBEAM SPLICING AREA. CORRECTIVE ACTION: REPAIRED PER ERA 612506-14AD. (0077678)SDR DALA2023112209638Unknown · unknownSHIP 3315 MTC WAS SCHEDULED TO REPLACE A CRACKED SIDE SEALING SECTION (DEPRESSOR) P/N F534753732140, BUT THEY DO NOT HAVE THE PARTS ON HAND TO ACCOMPLISH A PERMANENT REPAIR. THE DAMAGE WAS ORIGINALLY DEFERRED PER A330 SRM 53-00-29-300-002, WHICH ALLOWS CRACK DSDR REXA2024021500189Frame · corrodedFUSELAGE FRAME F.S.333 FROM STGR 26L TO STGR 26R IS CORRODED. REPAIRED FS333 LOWER FRAME SECTOR IAW CRJ 900 SRM 53-00-06-201-006-A01SDR HNAA2023121900488Unknown · unknownE010800 FRAME 25 CRACKED AT STRINGERS 15R-16R. FABRICATED AND INSTALLED “U” SHAPED DOUBER FOR REPAIR OF FRAME 25 AT STRINGERS 15R-16R IAW EMB145 SRM 53-00-04RE, ITEM 4, FIG 201 AND EO1-53-23-0429SDR DALA2023112209651Unknown · unknownCRACK ON UPPER RADIUS OF THE FRAME TAB OF THE OVERWING FRAME AT STA Y=674.000 RH OF 1.500 IN (REF. CARD 5310-01436-01D). SUMMARY OF NRC 00188: FRAME TAB OF THE OVERWING FRAME AT STA Y=674.000 RH WAS REPLACED PER B717-200 SRM 51-41-05-0G AND B717-200 SRM 51-41-SDR DALA2023112209650Unknown · unknownCRACK ON UPPER RADIUS OF THE FRAME TAB OF THE OVERWING FRAME AT STA Y=696.000 RH OF 1.500 IN (REF. CARD 5310-01436-01D). SUMMARY OF NRC 00189: FRAME TAB OF THE OVERWING FRAME AT STA Y=696.000 WAS REPLACED PER B717-200 SRM 51-41-05-0G AND SRM 51-41-02-0G; TOGETSDR DALA2023112209633Unknown · unknownSHIP 3119 CRACK INDICATION WAS FOUND ON FR16LH AT HOLE IDENTIFIED AS HOLE #6. CORRECTIVE ACTION: REPAIRED PER ERA 563227-14AD. (0075894)SDR DALA2023112209629Unknown · unknownSHIP 3120 CORROSION WEB FRAME 20 TO FR21 STR23 RH SIDE AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED WEB FRAME 20 TO FR 21 STR23 RH SIDE AT FWD GALLEY AREA AS PER A319 SRM 51-42-11 & A319 SRM 51-72-11. (0075691)SDR DALA2023112209634Unknown · unknownSHIP 3119 CRACK INDICATION WAS FOUND ON FR16RH AT HOLE IDENTIFIED AS HOLE #6. CORRECTIVE ACTION: REPAIRED PER ER/A 31-563226. (0075057)SDR DALA2023112109573Unknown · unknownCRACK ON FRAME BTW L7L AND STA Y1022 AT INTERNAL AFT FUSELAGE. SUMMARY OF NRC 00252: FRAME BTW L7L AND STA Y1022 AT INTERNAL AFT FUSELAGE WAS REPAIRED PER ERA 613218-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. (LP #0074650)SDR ASAA2023111949223Static Port · corrodedLH F/O AND LH CAPT STATIC PORTS WITH SIGNS OF CORROSION AROUND THE HOLES GROUNDED - YES. REMOVED AND REPLACED LH STATIC PORT REINFORCEMENT IAW A320-SRM-51-72-11, AIRBUS DWG: D53113482. OPS CHECK GOOD IAW A320-AMM-30-31-00-210-001-A. PROTECTIVE COATINGS WILL BESDR DALA2023112509677Unknown · unknownSHIP 3260 DISC: AD ERLATED 5311-01244-01B. R/H FR. 68 INTERNAL FRAME WEB HORIZONTAL FLANGE AT STGR 22 VISIBLE CRACK AT LOWER SURFACE. C/A: REPAIRED WEB IAW ER/A# 613584-14AD, REV O. (LP: 0073892)SDR DALA2023112009537Unknown · unknownSHIP 3260 DISC: ER/A 613584-14AD ISSUED FOR REPAIR AT RH FR68 WEB AT STOP 1. FOL LOW ON ACTION IS REQUIRED. C/A: PERFORM SECTION V EVERY 19700FC AFTER SECTION I. ASSOCIATED AA 5311-01244 ADDED FOR AC 3260 ASSOCIATED ER/A 14-613584 ADDED FOR AC 3260. (LP"\: 007SDR DALA2023112009536Unknown · unknownSHIP 3260 DISC: ER/A 613584-14AD ISSUED FOR REPAIR AT RH FRAME 68 WEB AT STOP 1. FOLLOW ON ACTION IS REQUIRED. C/A: PERFORM SECTION IV WITHIN 47300FC FROM SECTION I. SECTION IV MET HOD TBD PENDING STAGE III DAMAGE TOLERANCE EVALUTION ( DTE ). ER /A TO BE REVISSDR DALA2023112009535Unknown · unknownSHIP 3260 DISC: R/A 613584-14AD ISSUED FOR REPAIR AT RH FRAME 68 WEB AT STOP 1. FOLLOW ON ACTION IS REQUIRED. C/A: PERFORM SECTION III WITHIN 61500FC OF SECTION I. SECTION III MET HOD TBD PENDING STAGE III DAMAGE TOLERANCE EVALUATION ( DTE ). E R/A TO BE REVISSDR DALA2023112009534Unknown · unknownSHIP 3260 DISC: R/A 613584-14AD ISSUED FOR REPAIR INSTALLED AT RH FRAME 68 WEB, AT STOP 1. FOLLOW ACTION IS REQUIRED. C/A: PERFORM SECTION II WITHIN 37900FC FROM SECTION I. SECTION II MET HOD TBD AWAITING STAGE III DAMAGE TOLERANCE EVALUATION ( DTE ). ER/A TO SDR JJBA20231121013Unknown · unknownFWD FUSE II, FRAME 10 STR 9L ANGLE FOUND CRACKED. FWD FUSE II, FR10 STR 9L ANGLE REPLACED BY NEW ANGLESDR DALA2023112009541Unknown · unknownSHIP 3119 CORROSION FRAME 20 TO FR 21 INTERNAL SKIN LEVEL STR 42L IN AFT AVIONIC COMPARTMENT. CORRECTIVE ACTION: COMPLIED WITH ER/A 612896-14 REV. ORIGINAL. (0069897)SDR SWAA2023121322014Frame · elongatedAFT CARGO COMPARTMENT DOOR CUTOUT; AFT FRAME UPPER CORNER; PANEL PLATE HAS ELONGATED FASTENER HOLE.<[01] ACCOMPLISHED EA 23-153-03457 INSTRUCTIONS FOR ELONGATED HOLES AT AFT CARGO COMPARTMENT DOOR CUTOUT;[02] VERIFIED EA 23-153-03457 ACCOMPLISHEDSDR DALA2023112009518Unknown · unknownCRACK WAS FOUND ON THE CONTRAFRAME STRUCTURE OF THE AFT CABIN BULKHEAD DOOR. SUMMARY OF NRC 00362: COUNTERFRAME STRUCTURE WAS REPAIRED PER B717-200 SRM 51-70-11-2R PROCEDURE 1. (LP #0068675)SDR DALA2023111709483Unknown · unknownSHIP 1602 CABIN RH FRAME END FITTING ABOVE CENTER FULE TANK UPPER SURFACE AT STA 927 FOUND CRACK. CORRECTIVE ACTION: THE CRACKED RH FRAME END FITTING AT STA 927 REMOVED AND REPLACED AS PER B767-300 SRM 51-40-02 REV 121.00-APR-25-2023. (0067461)SDR DALA2023111609440Unknown · unknownCORROSION ON FRAME STA 889.0 BTW LONG 28RH TO 28LH AT AFT CARGO COMPARTMENT IN REF TO NRC 00254. SUMMARY OF NRC S/N 00654: CORROSION LEVEL 2. FRAME AT STA 889.0 BTW LONG 28RH TO 28LH AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717 SRM 53-20-07-2R REP. 3, 51-41-SDR REXA2024103101294Frame · corrodedFS 549 FRAME SECTOR IS CORRODED AT STGR 17L-18L REPAIRED FRAME SECTOR IAW CRJ900 SRM 53-00-06-201-001-A03SDR REXA2024103101293Frame · corrodedFRAME AT F.S. 533 STGR 17L TO STGR 18L IS CORRODED ON THE FWD AND AFT SIDE. REPAIRED FRAME AT F.S.533 IAW CRJ-900 SRM 53-00-06-201-001-A03SDR VNAA202401050001Frame · corrodedCORROSION ON FRAME FS= 310 BETWEEN STRG 27 TO 26RH AT MAIN AVIONICS COMPARTMENT. CORROSION ON FRAME FS= 310 BETWEEN STRG 27 TO 26RH AT MAIN AVIONICS COMPARTMENT WAS REPAIRED PER CRJ-900 SRM 53-00-06-201-005-A01.SDR YENA2023111701425Unknown · unknownDURING HEAVY MAINTENANCE: INITIAL INSPECTION: [CPCP FINDING] CORROSION ON FRAME 80 BTW STRG 28R/27R AT AFT CARGO DOOR CUTOUT STRUCTURE; (RESOLVED ON W/O: 1260255 TASKCARD: NR-00012 ) CORROSION ON FRAME 80 BTW STRG 26R/27R WAS EVALUATED OUT OF LIMITS, THEREFORE
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