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 DALA2024121611723Frame · dented(LOG 0707610) INITIAL INSPECTION:DENT ON FRAME UPPER STRUCTURE STA 500D AND STA 500C BTWN S25 L APROX. FRAME UPPER STRUCTURE STA 500D AND STA 500C BETWEEN S25 L APPROX WERE REPAIRED PER B737-800 SRM 53-30-07-2R-1.SDR FDEA202412131797Frame · crackedCENTER WING BOX - INSPECTION OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 LH SIDE, FASTENER "G" HOLE FOUND CRACK SIGNAL. COMPLIED WITH EA: 6-5710-T0381607 P1. TITLE: WINGS - BASIC WING STRUCTURE - LH WING FR47 REAR SPAR HOLE G CRACK REPAIRSDR WRXR20241213003Fitting · corrodedAT FS. 319 FRAME SPLICE FITTING HAS CORROSION PITTING. REPLACED SPLICE FITTING PN:SH670-31984-1 FS 319 STR 18R IAW CRJ 700 51-42-21-001-001-A01.SDR SWAA2025012976697Stub Frame · crackedCRACK INDICATION ON STUB FRAME LOCATED ON BS 296 BTW S-8R TO S-9R AT FWD GALLEY DOOR AREA CRACK LENGTH 0.187 IN. APPROX. AT PASSENGER CABIN 2024-758860<[01] REPLACED STUB FRAME LOCATED ON BS296 BTW STR 7R TO STR 10R AT FWD GALLEY DOOR AREA I.A.W B737-700 SRM 5SDR SWAA2025011376867Frame · crackedCRACKED FRAME AT PAX CABIN BS827 JUST BELOW S-8R. MARKED<[01] REPAIRED PER EA 24-153-03521;[02] CARD COMPLETE; AMT HAS ONE MEASUREMENT FIELD INCOMPLETE.;[03] ADDRESSED CORRECTIVE ACTION 2: COMPLETED MEASUREMENT FIELD.;[04] VERIFIED CORRECTIVE ACTION ITEMS; CARSDR DALA2024121311711Frame · crackedSHIP 5652 DTA MONITOR INSPECTION LOG REF ERA 622397-14 FUSELAGE / FRAME / STA 215.25 / S30-S29L / CRACK. CORRECTIVE ACTION: REF ERA 622397-14. (0707369)SDR DALA2024121311709Frame · damagedSHIP 3161 HOLES WERE FOUND OUT OF THE LIMITS OF STARTING DIAMETER. CORRECTIVE ACTION: REPAIRED PER ER/A 618674-14AD. (0706958)SDR DALA2024121311708Frame · damagedSHIP 3161 HOLES WERE FOUND OUT OF THE LIMITS OF STARTING DIAMETER. CORRECTIVE ACTION: REPAIRED PER ER/A 618674-14AD. (0706949)SDR DALA2024121311707Frame · damagedSHIP 3161 HOLES WERE FOUND OUT OF THE LIMITS OF STARTING DIAMETER. CORRECTIVE ACTION: REPAIRED PER ER/A 618674-14AD. (0706937)SDR DALA2024121311702Frame · wornWEAR AT FRAME OF STA Y=598 LH SIDE WAS FOUND OUT OF LIMITS. SUMMARY OF NRC 00716: FRAME OF STA Y=598 LH SIDE WAS REPAIRED PER ER/A 622297-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PER PRI 622297-14 REV 4. ASSOCIATED ER/A 14-622297 ADDED FOR AC 9543. (LP SDR SWAA2025011576322Frame · crackedCRACK FRAME LOCATED STA 440 AND BETWEEN STR 8R TO STR 9R AT PASSENGER CABIN 2024-759490<[01] REPAIRED FRAME LOCATED STA 440 AND BETWEEN STR 8R TO STR 9R AT PASSENGER CABIN IAW B737-700 EA#25-153-00006-WIP1 AND EA #25-153-00006. THIS REPAIR IS CLASSIFIED AS MAJSDR SWAA2025011576323Frame · crackedCRACK FRAME LOCATED STA 440 AND BETWEEN STR 8L TO STR 9L AT PASSENGER CABIN 2024-759491<[01] REPAIRED FRAME LOCATED STA 440 AND BETWEEN STR 8L TO STR 9L AT PASSENGER CABIN IAW B737-700 EA #24-153-03566-WIP1 AND EA #24-153-03566. THIS REPAIR IS CLASSIFIED AS MASDR SWAA2025011576327Frame · crackedCRACK FRAME LOCATED STA867 AND BETWEEN STR8R TO STR9R AT PASSENGER CABIN 2024-759492<[01] REPAIRED FRAME LOCATED STA867 AND BETWEEN STR8R TO STR9R AT PASSENGER CABIN IAW B737-700 EA #25-153-00018-WIP1 REV 2 AND EA #25-153-00018. THIS REPAIR IS CLASSIFIED AS MASDR SWAA2025011576320Frame · crackedCRACK FRAME LOCATED STA907 AND BETWEEN STR8R TO STR9R AT PASSENGER CABIN. REPAIRED FRAME LOCATED ON STA907 AND BETWEEN STR 7R TO STR 9R AT PASSENGER CABIN IAW EA: 24-153-03583-WIP1 AND EA SUMMARY 24-153-03583.SDR SWAA2025011576321Frame · crackedCRACK FRAME LOCATED STA 360 AND BETWEEN STR 8R TO STR 9R AT PASSENGER CABIN. REPAIRED FRAME LOCATED STA 360 AND BETWEEN STR 6R TO STR 9R AT PASSENGER CABIN IAW EA: 25-153-00022-WIP1 AND EA SUMMARY 25-153-00022.SDR AALA202412192166Door Frame · gougedAIRCRAFT IN BASE MAINTENANCE: R1 DOOR CUTOUT AT AFT FRAME, GUIDE FITTING IS GOUGED. REMOVED AND REPLACED R1 DOOR CUTOUT, AFT FRAME, GUIDE FITTING. PER B737-NG SRM 51-40-02-0G AND B737-NG AMM 20-50-11-910-801.SDR YENA2024121201548Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 RH SIDE, AT AFT GALLEY AREA, DOOR STOP 1, INBOARD/LOWER HOLE, CRACK INDICATION LOCATED AT 9 OCLOCK VIEW LOOKING FROM FWD, DEPTH IS 0.170 INCHES APPROX AEROMAN NR 2024-693521; (RESOLVED ON W/O: 1332046 TASKSDR CALA2024121803117Frame · crackedRH DOUBLE JOGGLE FR16 HOLE #6 HAS CRACK INDICATION IN FRAME LAYER. PERFORMED BUSHING REPAIR AT FR16 HOLE. PERFORMED BUSHING REPAIR AT FR16 HOLE #6 IAW SRM 53-11-12-300-012. REPAIR REQUIRES INITIAL INSPECTION #6 IAW SRM 53-11-12-300-012. REPAIR REQUIRES INITIASDR SWAA2024121674543Frame · buckledFOUND FRAME OUTBOARD CHORD BUCKLED AT BS 211.8 FROM S24R TO S-21R.<[01] REPAIRED DAMAGE PER EA 24-153-03387.SDR DALA2024120611489Frame · dentedSHIP 3134 FINDING DENT FRAME 53 AT LEVEL STR 33R IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS AS PER A319 SRM 53-00-12-300-004. (0695720)SDR DALA2024120511455Frame · crackedSHIP 3157 CRACK INDICATION FOUND IN OPEN FASTENER HOLE C LOCATED ON FRAME 16L JOGGLE AREA. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTION ON FASTENERS HOLE 7 LOCATED FUSELAGE FRAMES 16LH AT DOOR STOP NO. 1 AND 7 LEVEL DOUBLE JOGGLE AREA FASTENERS HOLES REPAIRSDR DALA2024120511454Fastener · crackedSHIP 3157 CRACK INDICATION FOUND IN OPEN FASTENER HOLE 7 LOCATED ON FRAME 16L JO GGLE AREA. CORRECTIVE ACTION: PERFORMED REPAIRINSTRUCTION ON FASTENERS HOLE 7 LOCATED FUSELAGE FRAMES 16LH AT DOOR STOP NO. 1 AND 7 LEVEL DOUBLE JOGGLE AREA FASTENERS HOLESREPAIR SDR SWIA2025010600038Frame · corrodedSEVERAL SMALL SPOTS OF CORROSION ON FRAME FLANGE ON THE FWD SIDE OF FS 605.00 SPANNING BETWEEN STGR 25L AND STGR 25R (FILED CLOSED) COMPLIED WITH REO 601R-53-61-8266 REV "--" DATED: 2024-12-14 SPLICE REPAIR TO FS605.00 LOWER FRAME SECTOR AT STR25R & STR SDR SWIA2025010600037Frame · corrodedCORROSION ON FRAME FLANGE ON THE FWD SIDE OF FS 589.00 BETWEEN STGR 20L AND STGR 21L (FILED CLOSED) PERFORMED REPAIR OF FRAME AND FUSELAGE SKIN ON BTW FS589.00 - FS605.00 AND BTW STR20L - STR27 WITH REFERENCE TO REO 601R-53-61-8267 REV "--" DATED 2024-12SDR SWIA202501061203Frame · corrodedCORROSION ON FRAME FLANGE ON THE FWD SIDE OF FS 559.00 +112 BETWEEN STGR 26L AND STGR 26R (FILE CLOSED) COMPLIED WITH REO 601R-53-51-698 DATED: 2024-12-07 REV-- REMOVED RIVETS AS NEEDED AND BLENDED SURFACE CORROSION ON FWD SIDE OF FRAME FLANGE AT FS559.00SDR SWIA20250103203Frame · corrodedCORROSION ON FRAME FLANGE ON THE FWD SIDE OF FS 559.00 +112 BETWEEN STGR 26L AND STGR 26R (FILE OPEN) COMPLIED WITH REO 601R-53-51-698 DATED: 2024-12-07 REV-- REMOVED RIVETS AS NEEDED AND BLENDED SURFACE CORROSION ON FWD SIDE OF FRAME FLANGE AT FS559.00 +SDR SWIA20250103009Frame · corrodedSEVERAL SMALL SPOTS OF CORROSION ON FRAME FLANGE ON THE FWD SIDE OF FS 605.00 SPANNING BETWEEN STGR 25L AND STGR 25R (FILED OPEN) COMPLIED WITH REO 601R-53-61-8266 REV "--" DATED: 2024-12-14 SPLICE REPAIR TO FS605.00 LOWER FRAME SECTOR AT STR25R & STR 26SDR SWAA2024123073853Frame · crackedCRACK ON FRAME LOCATED BS 259.5 BTW STR 8R TO STR 9R AT PASSENGER CABIN. REPAIRED FRAME - WEB AT BSTA 259.5 - BTW WL 240 & WL 280 AND BTW RBL 20 AND RBL 50 IAW EA 24-153-03393-WIP1; EA 24-153-03393-WIP2; AND EA 24-153-03393.SDR DALA2024120511480Frame · dentedSHIP 6704 AFT CARGO FRAME AT STA 1520 STR 26-27 LEFT DENT FOUND UNDER UPPER FLANGE. CORRECTIVE ACTION: TRIM OUT DENTED AREA ON FRAME STA 1520 BETWEEN S26L TO S25L IAW 757 SRM 53-00-07-2R, VERIFIED MATERIAL TO FABRICATE U CHANNEL, HEAT TREATED, FABRICATED LOCATSDR DALA2024120511479Frame · dentedSHIP 6704 AFT CARGO FRAME AT STA 1500 STR 26-27 LEFT HAND SIDE DENT FOUND UNDER UPPER FLANGE. CORRECTIVE ACTION: SUMMARY OF- TRIM OUT DENTED AREA ON FRAME 1500 BETWEEN SRT 26L TO STR 25L, VERIFIED MATERIAL ID 7075-O .071" PO # FS71436 TO FABRICATE U CHANNEL RESDR DALA2024120511478Frame · dentedSHIP 6704 AFT CARGO LEFT HAND FRAME AT STA 1440 STR 26-27 DENTS FOUND UNDER UPPER FLANGE. CORRECTIVE ACTION: SUMMARY OF- TRIM OUT DENTED AREA ON FRAME 1440 BETWEEN STR 25LTO STR 26L, VERIFIED MATERIAL TO FABRICATE U CHANNEL REPAIR, FABRICATED, HEAT TREATED, LOSDR DALA2024120511456Frame · crackedSHIP 3157 CRACK INDICATIONS FOUND IN HOLES #7 AND #C OF FR16 LHS DBL JOGGLE AREA. CORRECTIVE ACTION: REPAIRED PER ER/A 622681-14. (0691853)SDR DALA2024120411441Frame · crackedSHIP 3115 CRACK INDICATION ON FRAME 66 LH SIDE IN OPEN FASTENER HOLE LOWER INBO ARD OF DOOR STOP FITTING 1 POSITION. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON FRAME 66 LH SIDE ON FASTENER HOLES OF DOOR STOP FITTING 1 AS PER A319 SRM 53-41-12-300-008 SDR DALA2024120311395Cusp Web · corrodedCORROSION WAS FOUND ON LH CUSP ANGLE BTW STA Y=200-207 AT PASSENGER CABIN. SUMMARY OF NRC 00630: CORROSION LEVEL 2. LH CUSP ANGLE BTW STA Y=200-207 WAS REPAIRED PER B717 SRM 53-00-55-2R REPAIR 3. (LP #0690306)SDR DALA2024120311394Cusp Web · crackedCRACKED IN FIVE PLACES OF THE CUSP WEB MEMBRANE AT STA Y=266, STA X=-44.5; STA Y=589, STA X=-44.5; STA Y= 663, STA X=-44.5; STA Y=716, STA X=-44.5; AND STA Y=1012, STA X=-56. SUMMARY OF NRC 00472: (ET) (HFEC) INSPECTION WAS ACCOMPLISHED ONLY ON STA Y=663, STA SDR UIEA2024120301156Frame · misrepairedUNDOCUMENTED REPAIR ON FRAME WEB OF FWD CARGO COMPARTMENT AT STA 720, NEAR LBL 6.5 AND RBL 6.5.(<P>1. ACCOMPLISHED EL NO. T2024A53M-2904 REV.0. 2.JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR DALA2024120311393Cusp Web · corrodedCORROSION ON CUSP WEB BTW X=-56 TO X=-60 AND BTW STA Y=794-813 AT CPAX. SUMMARY OF NRC 00739: CORROSION LEVEL 2. CUSP WEB BTW X=-56 TO X=-60 AND BTW STA Y=794-813 AT CPAX WERE REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR PARAGRAPH 5 B (14) FIG 216.SDR K11A2025071700324Frame · crackedAFT CARGO PIT FRAME CRACKED. STA 767 CRACKED LS-25SDR SWIA2025022841130Frame · corrodedFS501 FRAME IS CORRODED ON THE ATTACHED FLANGE BETWEEN STR 26L & 26R (C-CHECK RO 2/26/2025) REMOVED AND INSTALLED NEW LOWER SECTOR FRAME @FS501.00 BETWEEN 26L AND 26R IAW CRJ900 SRM TASK 51-42-21-001-001-A01, SRM TSSK 51-42-06-001-001-A01 , BOMBARDIER SDR DALA2024120311430Frame · dentedSHIP 5652 DENT ON FRAME STA 1320 BTW STRG 27R AND 26R AT AFT CARGO COMP. CORRECTIVE ACTION: SUMMARY OF NRC 00640. FRAME STA 1320 BTW STRG 27R AND 26R AT AFT CARGO COMP WAS REPAIRED PER B757-200 SRM 53-00-07-2R PROCEDURE 5 REP. 5. (0686197)SDR DALA2024120311429Frame · dentedSHIP 5652 DENT ON FRAME STA 1320 BTW STRG 27R AND 26R AT AFT CARGO COMP. CORRECTIVE ACTON: SUMMARY OF NRC 00640. FRAME STA 1320 BTW STRG 27R AND 26R AT AFT CARGO COMP WAS REPAIRED PER B757-200 SRM 53-00-07-2R PROCEDURE 5 REP. 5. (0686190)SDR DALA2024120211373Door Frame · corrodedCORROSION ON ANGLE AND WEB ON LOWER DOOR JAMB STA Y=200 AT PAX CABIN (L1). SUMMARY OF NRC 00386: CORROSION LEVEL 2. ANGLE AND WEB ON LOWER DOOR JAMB STA Y=200 AT PAX CABIN WERE REPLACED PER B717-200 SRM 51-41-01-0G, 51-41-02-0G, 51-41-05-0G, AND 51-41-08-0G. (SDR CALA2024120202998Frame · corrodedB757-53-3-0526 AFT CARGO COMPT. STA 1440 S-29R AND S-30 FRAME HA S EXFOLIATED CORROSION ON THE LOWER WEB.SDR CALA2025012900233Frame · crackedFRAME 68 RH AFT FACE HAS CRACK INDICATION JUST BELOW STR 8 IN RA DIUS, APPROX .200 LONG, ALONG RADIUS JUST ABOVE UPPER SEAL FASTE NER. GEN BY V892444 ON HAECO LCQ NR 9296105 / 30105 CLEARING LP. FOR REPAIR, INSPECTION AND REFERENCE DETAILS, SEE NEW LP''S 36851SDR WX0A2024120432227Skin · dented(AIRCRAFT NOT GROUNDED) (DISCREPANCY NOTED DURING AIRCRAFT HEAVY MX VISIT) PERMANENT REPAIR PER EA 79-2024-184 NEED ACCOMPLISHED. DENT FWD FUSE AT FR21 +300MM, BELOW STR 23L / PERMANENT REPAIR PER EA 79-2024-184 ACCOMPLISHED. DENT FWD FUES AT FR21+300 MM BELOSDR DALA2024113011276Stringer · corrodedSHIP 3147 CORROSION LOWER SILL LOCATED AT LEVEL FR68 AND STR 23RH PASSENGER CABIN. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR LOC BETWEEN FR 67 TO FR 68 AT LEVEL STRINGER 23R LOWER SILL AREA PER A319 SRM 53-41-14. (0684475)SDR VNAA20250102002Stringer Splice · corrodedCORROSION ON SPLICE BETWEEN STGR 25RH AND STA. FS= 328.0 TO FS= 333.0 AT MAIN AVIONICS COMPARTMENT. (E/E) FOR EXCESSIVE DAMAGE ON SPLICE BETWEEN STGR 25RH AND STA. FS= 328.0 TO FS= 333.0 AT MAIN AVIONICS COMPARTMENT WAS FOUND OUT OF LIMITS PER CRJ-900 SRM 53-SDR SWAA2025010272574Frame · crackedCRACK ON FRAME LOCATED BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA 2024-728513<[01] TASK COMPLETED.<BR>PERFORMED REPAIR ON FRAME LOCATED BS312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA IAW EA-M-22-153-01244 MEASURE OF CRACK IS: L: 0.120 IN. TOOL USED: DIGITALSDR SWIA20241210128Frame · chafedEDGE OF FS 1162 BETWEEN STGR 6R AND 7R FOUND TO HAVE CHAFE DAMAGE (FILED CLOSED) REPAIRED CHAFE DAMAGE TO THE FRAME AT FS1162.00 BETWEEN STGR 6R AND 7R IN REF TO REO 690-53-71-081 REV -- DATED 2024-12-10. COMPLIED WITH TASK CARD 51-900-1002-SKY SRUCTURALSDR DALA2024120211347Frame · crackedSHIP 6703 AFT CARGO L/H SIDE FUSELAGE FRAME HAS EXISTING REPAIR AT FRAME STA 1460 S26L. APPROX 12" IN LENGTH. REF AD TASK CARD 5311-01227 -01A. STEP # 2. CORRECTIVE ACTION: SUMMARY OF NR-00205- REMOVED, FABRICATED AND INSTALLED FRAME REPAIR AT STA 1460 FRAME B
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